EP 3190051 B1 20190619 - ENHANCED PERFORMANCE JET ENGINE MOUNTING STRUTS
Title (en)
ENHANCED PERFORMANCE JET ENGINE MOUNTING STRUTS
Title (de)
STRAHLTRIEBWERKSMONTAGESTREBEN MIT VERBESSERTER LEISTUNG
Title (fr)
PYLÔNES HAUTES PERFORMANCES DE FIXATION DE RÉACTEUR
Publication
Application
Priority
US 201614990697 A 20160107
Abstract (en)
[origin: EP3190051A1] In one example embodiment, a strut (14) for mounting a jet engine (10) to a wing (12) of an aircraft includes a plurality of engine mounts (312, 316) and a space frame truss (600) supported from the wing (12) and comprising front and aft portions, the front portion (602) being coupled to and supporting the engine mounts (312, 316), the aft portion (604) extending upwardly and rearwardly from an aft end of the front portion (602). By removing the aft end of the strut (14) from the core exhaust zone (20) of the engine (10), substantial reductions in the weight and drag of the strut (14), and a corresponding increase in the specific fuel consumption of the associated aircraft may be achieved.
IPC 8 full level
B64D 27/26 (2006.01)
CPC (source: CN EP RU US)
B64D 27/18 (2013.01 - CN); B64D 27/40 (2024.01 - EP RU US); B64D 27/402 (2024.01 - US); Y02T 50/40 (2013.01 - EP US)
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
DOCDB simple family (publication)
EP 3190051 A1 20170712; EP 3190051 B1 20190619; BR 102016029834 A2 20170919; BR 102016029834 B1 20221227; CN 107054670 A 20170818; CN 107054670 B 20211221; EP 3524525 A1 20190814; EP 3524525 B1 20201007; JP 2017165394 A 20170921; JP 6920054 B2 20210818; RU 2016142738 A 20180503; RU 2016142738 A3 20200217; RU 2729129 C2 20200804; US 10118709 B2 20181106; US 2017197723 A1 20170713; US 2018170562 A1 20180621; US 9896217 B2 20180220
DOCDB simple family (application)
EP 16196057 A 20161027; BR 102016029834 A 20161219; CN 201611120507 A 20161205; EP 19167428 A 20161027; JP 2016247351 A 20161221; RU 2016142738 A 20161031; US 201614990697 A 20160107; US 201815892334 A 20180208